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Effects of syngas composition on combustion induced vortex breakdown (CIVB) flashback in a swirl stabilized combustor

机译:合成气成分对涡流稳定燃烧室中燃烧诱发的涡旋破裂(CIVB)闪回的影响

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摘要

Flame flashback attributed to combustion induced vortex breakdown (CIVB) is a major design challenge for swirl stabilized burner combustors. This paper presents an experimental investigation of combustion induced vortex breakdown (CIVB) flashback propensity for flames yielded from Hydrogen (H_2)-Carbon Monoxide (CO) fuel blends and actual synthesized gas (syngas) mixtures. A two-fold experimental approach, consisting of a high definition digital imaging system and a high speed PIV system, was employed. The main emphasis was on the effect of concentration of different constituents in fuel mixtures on flashback limit. In addition, the effect of Swirl Number on flashback propensity was discussed. The percentage of H_2 in fuel mixtures played the dominant role when CIVB flashback occurred. For a given air mass flow rate, the mixture containing a higher percentage of H_2 underwent flashback at much leaner conditions. Flashback maps for actual syngas fuel compositions showed a distinct behavior when various concentrations of diluents were introduced in the mixture. For the two major diluents tested, carbon dioxide (CO_2) and nitrogen dioxide (NO_2), CO_2 was more dominant. The effect of Swirl Number on the flashback propensity was also tested and showed a decrease with an increase in Swirl Number. The final portion of this paper also provides an analysis of flow field of reacting flames which revealed complex vortex-chemistry interactions leading to vortex breakdown and flashback. Based on the experimental results a parametric model similar to Peclet Number approach was developed employing a flame quenching concept. A value of the quench parameter, C_(quench) was obtained from the correlation of flow Peclet Number and flame Peclet Number, which was observed to be dominated by the fuel composition rather than Swirl Number.
机译:归因于燃烧引起的涡旋破坏(CIVB)的火焰回火是涡旋稳定燃烧器燃烧室的主要设计挑战。本文提供了一种实验研究,研究了氢(H_2)-一氧化碳(CO)燃料混合物和实际合成的气体(合成气)混合物产生的火焰的燃烧诱导的涡旋破裂(CIVB)回火倾向。采用了由高清晰度数字成像系统和高速PIV系统组成的双重实验方法。主要重点是燃料混合物中不同成分的浓度对闪回极限的影响。此外,还讨论了旋流数对回火倾向的影响。当CIVB闪回发生时,燃料混合物中H_2的百分比起主导作用。对于给定的空气质量流量,含有更高百分比的H_2的混合物会在更稀薄的条件下经历反燃。当在混合物中引入各种浓度的稀释剂时,实际合成气燃料成分的闪回图显示出不同的行为。对于测试的两种主要稀释剂,二氧化碳(CO_2)和二氧化氮(NO_2),CO_2更具优势。还测试了旋流数对回火倾向的影响,并显示出随着旋流数的增加而降低。本文的最后部分还提供了对反应火焰流场的分析,揭示了复杂的旋涡-化学相互作用导致旋涡破裂和回火。根据实验结果,采用火焰猝灭概念开发了类似于Peclet数方法的参数模型。淬火参数的值C_(淬火)是从流量佩克雷特数和火焰佩克雷特数的相关性获得的,据观察,该相关性由燃料成分而不是涡旋数决定。

著录项

  • 来源
    《Fuel 》 |2011年第11期| p.3274-3284| 共11页
  • 作者单位

    NASA Center for Space Exploration Technology Research (cSETR), Department of Mechanical Engineering, The University of Texas at El Paso, El Paso, TX 79968, USA;

    NASA Center for Space Exploration Technology Research (cSETR), Department of Mechanical Engineering, The University of Texas at El Paso, El Paso, TX 79968, USA;

    NASA Center for Space Exploration Technology Research (cSETR), Department of Mechanical Engineering, The University of Texas at El Paso, El Paso, TX 79968, USA;

    NASA Center for Space Exploration Technology Research (cSETR), Department of Mechanical Engineering, The University of Texas at El Paso, El Paso, TX 79968, USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    syngas fuels; lean premixed combustion; swirl flow; flame flashback; combustion induced vortex breakdown; (civb);

    机译:合成气燃料;稀薄的预混燃烧;旋流火焰回火燃烧引起的涡流破坏;(civb);

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